STARLINER CALYPSO 1, 59968 (Decayed)
Orbit data source: Space-Track
STARLINER CALYPSO 1, 59968 was an American payload satellite in LEO that was launched on Wed, 05 Jun 2024 UTC via an ATLAS V N22 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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59968 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Boeing C3PF
Mission
Decayed spacecraft
Bus & Motor
CST-100, Unknown motor
Mass
8,000 kg wet, 8,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 STARLINER CALYPSO 1
1 59968U 24109A 24253.87704602 .00012401 00000-0 23421-3 0 9996
2 59968 51.6395 255.8321 0007834 334.1073 94.7593 15.48815630471007Epoch: 2024-09-09T21:02Z
TLE epoch observation values (Epoch: 2024-09-09T21:02:56.776Z)
Latitude
47.18903°
Longitude
8.86614°
Altitude
425.642 km
Speed
7.662 km/s
True Right ascension
20h 56m 00s
True Declination
47° 00' 33"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
16:47:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
426.024 km
Perigee altitude
415.371 km
Semi-major axis
6,798.834 km
Eccentricity
0.00078
Inclination
51.6395°
RAAN
255.8321°
Arg. of periapsis
334.1073°
True anomaly
94.84875°
Mean anomaly
94.7593°
Eccentric anomaly
94.80403°
Mean motion
3.87161 °/min
Orbital period
92.98 mins
BSTAR
0.00023421
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Other satellites on launch #109 in the year 2024 (2024-06-05 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.STARLINER CALYPSO 1 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-17 00:38:17.597Z | 283.665° WNW | 2025-09-17 00:40:17.597Z | 324.783° NNW | 20.224° | 2025-09-17 00:42:17.597Z | 16.81° NNE |
| 4 mins | 2025-09-17 05:30:17.597Z | 330.551° NNW | 2025-09-17 05:31:17.597Z | 20.706° NNE | 39.769° | 2025-09-17 05:34:17.597Z | 114.022° SE |
| 4 mins | 2025-09-17 23:41:17.597Z | 284.589° WNW | 2025-09-17 23:42:17.597Z | 326.03° NNW | 31.487° | 2025-09-17 23:45:17.597Z | 39.442° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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